View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57696U 26145.61203919 +.00000000 +00000-0 +29358-3 0 00005
2 57696 97.5549 239.7247 0012673 60.9079 299.3418 15.10390433 03
| Epoch (UTC): | 25 May 2026 14:41:20 |
| Eccentricity: | 0.0012673 |
| inclination: | 97.5549° |
| perigee height: | 526 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 239.7247° |
| argument of perigee: | 60.9079° |
| revolutions per day: | 15.10390433 |
| mean anomaly at epoch: | 299.3418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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